System for the closed loop estimation of linear models entrance output of a wind turbine. (Machine-translation by Google Translate, not legally binding)
System for the closed-loop estimation of linear models input output of a wind turbine, which consists of applying a reference signal (5) and a known excitation signal (7), in a real wind turbine (1) and in an estimated model of wind turbine (1b), which are controlled in closed loop by a controller (...
Gespeichert in:
Hauptverfasser: | , , |
---|---|
Format: | Patent |
Sprache: | eng ; spa |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Zusammenfassung: | System for the closed-loop estimation of linear models input output of a wind turbine, which consists of applying a reference signal (5) and a known excitation signal (7), in a real wind turbine (1) and in an estimated model of wind turbine (1b), which are controlled in closed loop by a controller (2) fed with the output (6) and other variables (9) of the wind turbine (1) and with the output (6b) of the estimated model (1b), so that from the comparison of the output signals of the wind turbine (1) and the estimated model (1b), values (8) are obtained that are analyzed through a parametric adaptation algorithm (4), providing values that make up the estimated wind turbine model (1b). (Machine-translation by Google Translate, not legally binding)
Sistema para la estimación en lazo cerrado de modelos lineales entrada salida de un aerogenerador, que consiste en aplicar una señal de referencia (5) y una señal de excitación (7) conocida, en un aerogenerador real (1) y en un modelo estimado de aerogenerador (1b), los cuales están controlados en lazo cerrado por un controlador (2) alimentado con la salida (6) y otras variables (9) del aerogenerador (1) y con la salida (6b) del modelo estimado (1b), de manera que de la comparación de las señales de salida del aerogenerador (1) y del modelo estimado (1b) se obtienen unos valores (8) que son analizados a través de un algoritmo de adaptación paramétrica (4), proporcionando unos valores que configuran el modelo estimado de aerogenerador (1b). |
---|